@inproceedings{oai:jaxa.repo.nii.ac.jp:00006564,
 author = {徳川, 直子 and 吉田, 憲司 and 高木, 正平 and Tokugawa, Naoko and Yoshida, Kenji and Takagi, Shohei},
 book = {宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集　第33回・第34回, JAXA Special Publication: Proceedings of the 33rd and 34th JAXA Workshops on Investigation and Control of Boundary-Layer Transition},
 month = {Jan},
 note = {Measurement system of supersonic boundary-layer transition for the SST experimental airplane (NEXST-1) is evaluated for successful capture of transition signature prior to the flight test. Output levels of hot-film sensors and unsteady pressure transducers at the flight test are estimated on the basis of experimental results obtained in ground facilities and are found to be significantly above electric noise level in transitional state. Estimation shows that transition point with the maximum values of shear-stress and pressure fluctuations in the chordwise direction is inferred to be detectable., 資料番号: AA0047776010, レポート番号: JAXA-SP-04-002},
 pages = {31--32},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {SSTロケット実験機の遷移計測にむけて},
 volume = {JAXA-SP-04-002},
 year = {2005}
}